  NACA 0012 : INPUT FOR (CAS2D)
  XCELL = 0.24000D+02YCELL = 0.06000D+02PMESH = 4.00000D+00
  ALPHA1= 0.00000D+02TWIST =-0.00000D+02ALPHA2= 0.00000D+02
  PITCH = 3.60000D+00RO1   = 0.01580D+00RO2   = 0.00050D+00
  FMACH = 0.80000D+00RLX   = 1.72000D+00AR    = 1.00000D+00
  TITR1 = 2.00000D+02TITR2 = 2.00000D+02TITR3 = 2.00000D+02
  POINTS= 0.64000D+02GAMMA = 1.40000D+00CONVER= 1.00000D-08
  1.000000  0.000000
  0.991149 -0.001249
  0.988699 -0.001592
  0.986111 -0.001953
  0.983246 -0.002352
  0.979970 -0.002806
  0.976153 -0.003333
  0.971670 -0.003949
  0.966402 -0.004668
  0.960239 -0.005504
  0.953082 -0.006466
  0.944839 -0.007564
  0.935430 -0.008805
  0.924789 -0.010191
  0.912861 -0.011724
  0.899603 -0.013402
  0.884988 -0.015223
  0.869002 -0.017178
  0.851644 -0.019261
  0.832929 -0.021459
  0.812885 -0.023761
  0.791554 -0.026150
  0.768990 -0.028611
  0.745260 -0.031125
  0.720445 -0.033673
  0.694635 -0.036234
  0.667930 -0.038784
  0.640441 -0.041301
  0.612286 -0.043758
  0.583589 -0.046131
  0.554482 -0.048392
  0.525097 -0.050515
  0.495574 -0.052472
  0.466051 -0.054236
  0.436667 -0.055781
  0.407559 -0.057084
  0.378862 -0.058123
  0.350707 -0.058879
  0.323218 -0.059337
  0.296513 -0.059486
  0.270703 -0.059320
  0.245888 -0.058838
  0.222159 -0.058043
  0.199595 -0.056946
  0.178263 -0.055559
  0.158219 -0.053903
  0.139504 -0.052000
  0.122147 -0.049876
  0.106161 -0.047560
  0.091546 -0.045084
  0.078288 -0.042480
  0.066359 -0.039781
  0.055718 -0.037019
  0.046310 -0.034225
  0.038067 -0.031425
  0.030909 -0.028645
  0.024747 -0.025901
  0.019479 -0.023200
  0.014995 -0.020537
  0.011178 -0.017879
  0.007902 -0.015155
  0.005038 -0.012202
  0.002449 -0.008591
  0.000000  0.000000
  GOSTELOW CUSPED AIRFOIL CASCADE : INPUT FOR (CAS2D)
  XCELL = 0.24000D+02YCELL = 0.06000D+02PMESH = 4.00000D+00
  ALPHA1= 0.53500D+02TWIST =-0.37500D+02ALPHA2= 3.00249D+01
  PITCH = 9.90157D-01RO1   = 0.01280D+00RO2   = 0.00005D+00
  FMACH = 0.00100D+00RLX   = 1.75000D+00AR    = 1.00000D+00
  TITR1 = 2.00000D+02TITR2 = 2.00000D+02TITR3 = 1.00000D+02
  POINTS= 0.87000D+02GAMMA = 1.40000D+00CONVER= 1.00000D-07
  0.999991  0.000000
  0.998595  0.000385
  0.994593  0.001443
  0.988072  0.003086
  0.979082  0.005228
  0.967645  0.007784
  0.953763  0.010667
  0.937419  0.013788
  0.918575  0.017052
  0.897176  0.020363
  0.873147  0.023617
  0.846384  0.026703
  0.816756  0.029505
  0.784086  0.031892
  0.748138  0.033724
  0.708586  0.034839
  0.691659  0.035043
  0.664964  0.035048
  0.616568  0.034120
  0.562254  0.031742
  0.499957  0.027440
  0.425136  0.020330
  0.321980  0.007784
  0.270853  0.000795
  0.247212 -0.002507
  0.232032 -0.004626
  0.178493 -0.011872
  0.165366 -0.013534
  0.146439 -0.015791
  0.145132 -0.015940
  0.110982 -0.019354
  0.057582 -0.021491
  0.030894 -0.019222
  0.015190 -0.015098
  0.005986 -0.009925
  0.001248 -0.004101
  0.000063 -0.000393
 -0.000141  0.002144
  0.001131  0.008657
  0.004615  0.015335
  0.009997  0.022098
  0.017058  0.028887
  0.025639  0.035653
  0.035627  0.042358
  0.046942  0.048966
  0.059532  0.055447
  0.073366  0.061772
  0.088437  0.067915
  0.104755  0.073846
  0.122350  0.079540
  0.141277  0.084966
  0.161613  0.090091
  0.183466  0.094877
  0.184036  0.094993
  0.206986  0.099281
  0.232276  0.103250
  0.245855  0.105050
  0.259913  0.106714
  0.274603  0.108231
  0.289989  0.109585
  0.306148  0.110761
  0.323177  0.111738
  0.341198  0.112491
  0.360367  0.112988
  0.380891  0.113186
  0.403055  0.113028
  0.427269  0.112434
  0.454158  0.111280
  0.484771  0.109361
  0.521145  0.106282
  0.568504  0.101040
  0.594192  0.097637
  0.650079  0.088934
  0.710527  0.077591
  0.763025  0.066180
  0.786059  0.060733
  0.826604  0.050519
  0.855912  0.042661
  0.879212  0.036150
  0.929087  0.021530
  0.941336  0.017826
  0.951990  0.014578
  0.961258  0.011740
  0.969296  0.009275
  0.987109  0.003833
  0.998683  0.000378
  0.999991  0.000000
